Turbine airfoil cooling system with axial flowing serpentine...

Fluid reaction surfaces (i.e. – impellers) – With heating – cooling or thermal insulation means – Changing state mass within or fluid flow through working...

Reexamination Certificate

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

C415S115000

Reexamination Certificate

active

07549843

ABSTRACT:
A cooling system for a turbine airfoil of a turbine engine having suction and pressure side serpentine cooling channels formed between an internal support core and an outer wall of the turbine airfoil. The suction and pressure side serpentine cooling channels may be formed from legs extending in a general chordwise direction between leading and trailing edges of the airfoil. The suction and pressure side serpentine cooling channels may receive cooling fluids from a cooling fluid supply source through a cooling fluid inlet, pass the cooling fluids through the cooling system and exhaust the cooling fluids through a cooling fluid exhaust orifice proximate to the tip section. The cooling system is particularly suitable for use with low cooling fluid flow.

REFERENCES:
patent: 3736071 (1973-05-01), Kydd
patent: 3849025 (1974-11-01), Grondahl
patent: 4118145 (1978-10-01), Stahl
patent: 5536143 (1996-07-01), Jacala et al.
patent: 5820337 (1998-10-01), Jackson et al.
patent: 5967752 (1999-10-01), Lee et al.
patent: 5971708 (1999-10-01), Lee
patent: 6099252 (2000-08-01), Manning et al.
patent: 6709230 (2004-03-01), Morrison et al.
patent: 6832889 (2004-12-01), Lee et al.
patent: 6902372 (2005-06-01), Liang
patent: 6957949 (2005-10-01), Hyde et al.
patent: 6981840 (2006-01-01), Lee et al.
patent: 2005/0008487 (2005-01-01), Lee et al.
patent: 2005/0111976 (2005-05-01), Lee
patent: 2005/0129508 (2005-06-01), Fried et al.
patent: 2005/0169752 (2005-08-01), Lee et al.
patent: 2005/0226726 (2005-10-01), Lee et al.

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Turbine airfoil cooling system with axial flowing serpentine... does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Turbine airfoil cooling system with axial flowing serpentine..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Turbine airfoil cooling system with axial flowing serpentine... will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-4125880

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.